== √ME 5463-001 Fracture Mechanics, Final Exam #3 == --- //[[honeypot@handbasket.org|David Wagner]] 2009/12/08 16:52// A thin-walled __cylindrical__ pressure container (70 mm inner diameter and 90 mm outer diameter) has a semicircular surface flaw (//a// = 1.5 mm), which is oriented normal to the longitudinal direction of the cylinder. If the maximum pressure is 55 MPa and the minimum pressure is 20 MPa, estimate the number of pressure cycles the cylinder could withstand before failure. Assume that da/dN = 5*10^{-39} (Delta K)^4, the fracture toughness of the material is 20.9 MPa√m. Note this is //not// the worst case. A crack oriented //parallel// to the longitudinal direction would have twice the opening stress applied. * //Assume the plate is approximately flat with infinite x- and y-dimensions around the crack.// ====== Given ====== * //r// = 0.090 //m//; * //t// = 0.020 //m//; * p_max = 55*10^6 Pa; * a_0 = 0.0015 //m//; * K_c = 20.9*10^6 //Pa√m//; * {da}/{dN} = 5*10^{-39} (Delta K)^4 = A(Delta K)^m. ====== Found ====== * Hoop Stress: sigma_x = {pr}/t (does not introduce singular stresses at the crack tip). * Longitudinal Stress: sigma_y = {pr}/{2t}; * There are no shear stresses. * Y approx (1.12)(0.64) = 0.7168. //Edge condition making half of a penny crack.// ====== Determined ====== * A = 5*10^{-39}; * //m// = 4; * Delta p = 35*10^6 Pa; * p_mean = {55+20}/2 = 37.5*10^6 Pa; * p_amp = 17.5*10^6 Pa. * sigma_max = {55*10^6 * 0.090}/{2*0.020}=123.750 *10^6 Pa The crack length at brittle failure will be: a_f = {1/pi} ({K_c}/{Y sigma_max})^2 =a_f = {1/pi} ({20.9*10^6}/{0.7168 * 123.75*10^6})^2 =0.043636 //m//. Delta sigma =Delta sigma_y = {Delta p r}/{2t} ={35*10^6 * 0.090}/{2 * 0.020} = 78.75*10^6 //Pa// N_f = 2 { {a_0}^{{2-m}/2} - {a_f}^{{2-m}/2} } / {(m-2)A(Y sqrt{pi} Delta sigma)^m} = 2 { {a_0}^{-1} - {a_f}^{-1} } / {2 A(Y sqrt{pi} Delta sigma)^4} = { {0.0015}^{-1} - 0.043636^{-1} } / {5*10^{-39} * 0.7168^4 * pi^2 * {78.75*10^6}^4} =1.2849*10^9 cycles. ^1.3 Billion Cycles^